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Normalized solutions of Schrödinger equations involving Moser-Trudinger critical growth

  • Gui-Dong Li and Jianjun Zhang EMAIL logo
Published/Copyright: July 2, 2024

Abstract

In this article, we are concerned with the nonlinear Schrödinger equation

Δ u + λ u = μ u p 2 u + f ( u ) , in R 2 ,

having prescribed mass

R 2 u 2 d x = a 2 > 0 ,

where λ arises as a Lagrange multiplier, μ > 0 , p ( 2 , 4 ] , and the nonlinearity f C 1 ( R , R ) behaves like e 4 π u 2 as u + . For a L 2 -critical or L 2 -subcritical perturbation μ u p 2 u , we investigate the existence of normalized solutions to the aforementioned problem. Moreover, the limiting profiles of solutions have been considered as μ 0 or a 0 . This result can be considered as a supplement to the work of Soave (Normalized ground states for the NLS equation with combined nonlinearities: the Sobolev critical case, J. Funct. Anal. 279 (2020), no. 6, 1–43) and Alves et al. (Normalized solutions for a Schrödinger equation with critical growth in R N , Calc. Var. Partial Differential Equations 61 (2022), no. 1, 1–24).

MSC 2010: 35J20; 35B33; 35B45

1 Introduction

Soave [31] considered the existence and properties of ground-states for the nonlinear Schrödinger equation with combined power nonlinearities

Δ u = λ u + μ u q 2 u + u p 2 u , in R N , N 1 ,

having prescribed mass

R N u 2 d x = a 2 ,

under different assumptions on a > 0 , μ R , and

2 < q 2 + 4 N p < 2 * , q p ,

i.e., the two nonlinearities have different characters with respect to the L 2 -critical exponent p ¯ 2 + 4 N . The cases p > p ¯ and p < p ¯ are called the mass L 2 -supercritical and mass L 2 -subcritical, respectively. Here and in what follows, 2 * denotes the critical exponent for the Sobolev embedding H 1 ( R N ) L p ( R N ) (i.e., 2 * = 2 N ( N 2 ) if N 3 and 2 * = if N = 1 , 2 ). Subsequently, Soave extends these results to the Sobolev critical case in [32], where the author considered

(1.1) Δ u = λ u + μ u q 2 u + u 2 * 2 u , in R N , N 3 ,

having prescribed mass

R N u 2 d x = a 2 > 0 .

For a L 2 -subcritical, L 2 -critical, of L 2 -supercritical perturbation μ u q 2 u , existence/non-existence and stability/instability results are obtained in [32]. This can be considered as a counterpart of the Brézis-Nirenberg problem in the context of normalized solutions and seems to be the first contribution regarding existence of normalized ground-states for the Sobolev critical Schrödinger equation in the whole space R N . It is worth noting that when N 4 , 2 < q < 2 + 4 N , the existence of a second solution was proposed in [32] as an open problem. Motivated by this question, Jeanjean and Le proved that there also exist standing waves that are not ground-states and are located at a mountain-pass level of the energy functional in [18], which gives a positive answer to the question raised by Soave in [32]. In addition, when

N 3 , 2 + 4 N q < 2 * ,

Soave showed that the existence of solutions to Problem (1.1) also depends on additional assumptions on a and μ . Li in [25] also studied this case and then proved the existence of normalized ground-states, using the Pohožaev constraint, Schwartz symmetrization rearrangements, and various scaling transformations. Moreover, when 2 + 4 N < q < 2 * , Li showed that the existence of solutions does not depend on additional assumptions on a and μ . Meanwhile, [2,38] investigated the situation where the existence of solutions occurs under these conditions. In particular, in [2], the authors also studied the exponential critical growth for N = 2 , namely,

(1.2) Δ u = λ u + f ( u ) , in R 2 ,

having prescribed mass

R 2 u 2 d x = a 2 > 0 ,

where f satisfies

  1. lim t 0 f ( t ) t τ = 0 as t 0 , for some τ > 3 , and

    lim t + f ( t ) e α t 2 = 0 , for α > 4 π , + , for 0 < α < 4 π ,

  2. there exists a positive constant θ > 4 such that

    0 < θ F ( t ) t f ( t ) , for all t 0 , where F ( t ) = 0 t f ( s ) d s ,

  3. there exist constants p > 4 and μ > 0 such that

    sgn ( t ) f ( t ) μ t p 1 , for all t 0 ,

    where sgn : R \ { 0 } R is given by

    sgn ( t ) = 1 , if t > 0 , 1 , if t < 0 ,

  4. let F ˜ ( t ) = f ( t ) t 2 F ( t ) for all t R and f C 1 ( R ) , F ˜ ( t ) exists and F ˜ ( t ) t 4 F ˜ ( t ) , for all t R .

They show that Problem (1.2) admits a couple ( u , λ ) H 1 ( R 2 ) × R of weak solutions for all μ μ * . Moreover, if ( f 4 ) is also assumed and f is odd, then the solutions can be chosen as a positive ground-state solution of Problem (1.2) on the sphere

(1.3) S ( a ) = u H 1 ( R 2 ) : R 2 u 2 d x = a 2 .

Here, we point out that in [2], they require a ( 0 , 1 ) . Subsequently, the authors in [10] got rid of condition ( f 2 ) and show that this result is still true. For more related results on normalized solutions of nonlinear Schrödinger equations, we refer to [1,35,11,12, 16,17,19, 20,24,29, 30,36,37, 40,41] and references therein.

Inspired by the aforementioned works, we aim to extend Soave’s results in [31,32] to the exponential critical case. Moreover, one can see that ( f 3 ) implies that f is L 2 -supcritical growth. So, the main purpose of this article is to seek normalized solutions of Problem (1.2) involving L 2 -subcritical or L 2 -critical perturbations. Precisely, we consider the following Schrödinger equation:

(P) Δ u + λ u = μ u p 2 u + f ( u ) , in R 2 ,

having prescribed mass

R 2 u 2 d x = a 2 > 0 ,

where μ > 0 , p ( 2 , 4 ] , λ R arises as a Lagrange multiplier, and a > 0 is a given constant. We assume that f satisfies the following conditions:

  1. f C 1 ( R , R ) is odd,

  2. lim t 0 f ( t ) t τ = 0 as t 0 , for some τ > 3 , and there exists C , T > 0 such that for

    f ( t ) C e 4 π t 2 , t > T ,

  3. there exist constants q > 4 , θ > 4 , and κ > 0 such that F ( t ) κ t q , for all t R , and

    0 < θ F ( t ) t f ( t ) , for all t 0 , where F ( t ) = 0 t f ( s ) d s ,

  4. let K ( t ) = f ( t ) t 2 F ( t ) and the function t K ( t ) t 4 K ( t ) t p is strictly increasing in ( 0 , ) .

We look for solutions of problem ( P ) having a prescribed L 2 -norm, which are often referred to as normalized solutions. More precisely, for given a > 0 , we look for a couple of solution ( u a , λ a ) H 1 ( R 2 ) × R to problem ( P ) with

R 2 u 2 d x = a 2 .

This type of solution can be obtained by looking for critical points of the following functional E μ : H 1 ( R 2 ) R :

E μ ( u ) = 1 2 R 2 u 2 d x μ p R 2 u p d x R 2 F ( u ) d x

on the constraint

(1.4) S ( a ) = u H 1 ( R 2 ) : R 2 u 2 d x = a 2 .

It is clear that for each critical point, u a S ( a ) of E μ S ( a ) corresponds to a Lagrange multiplier λ a R such that ( u a , λ a ) solves problem ( P ).

In Section 3, one explicit value μ 0 > 0 is given such that, for any μ ( 0 , μ 0 ) , there exists a set V ( a ) S ( a ) having the property that

m μ ( a ) inf u V ( a ) E μ ( u ) < 0 < inf u V ( a ) E μ ( u ) .

The sets V ( a ) and V ( a ) are given by

V ( a ) { u S ( a ) : u 2 2 < ρ 0 } and V ( a ) { u S ( a ) : u 2 2 = ρ 0 }

for a suitable ρ 0 > 0 . Our results state as follows.

Theorem 1.1

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold, then there exist μ 0 > 0 such that problem ( P ) has a positive and radial ground-state solution for any 0 < μ < μ 0 . This ground-state is a (local) minimizer of E μ in the set V ( a ) . In addition, any ground-state for E μ on S ( a ) is a local minimizer of E μ on V ( a ) . Moreover, there exists κ 0 > 0 such that, for any κ κ 0 , where κ is given in ( f 7 ) , problem ( P ) has a second solution v S ( a ) , which is the mountain path-type solution and satisfies E μ ( v ) > 0 .

Theorem 1.2

Let p = 4 and ( f 5 ) ( f 8 ) hold, then there exists a 1 > 0 , μ 1 > 0 , and κ 1 > 0 such that E μ restricted to S ( a ) has a ground-state solution if 0 < μ < μ 1 and κ > κ 1 , or 0 < a < a 1 and κ > κ 1 , which is the mountain path-type solution.

Theorem 1.3

Assume that 2 < p 4 and ( f 5 ) ( f 8 ) hold. Let u μ , a be the positive and radial ground-state solution in Theorem 1.1. Set v μ and w a , μ as the mountain path-type solution in Theorems 1.1and 1.2, respectively. Then, the following assertions hold:

  1. u μ , a 2 0 and the corresponding Lagrange multiplier λ μ , a 0 as μ 0 + ,

  2. u μ , a 0 , in H 1 ( R 2 ) and λ μ , a 0 as a 0 + . Let U be the unique positive solution of

    (1.5) Δ U + U = μ U p 1 , in R 2 , lim x U ( x ) = 0 ,

    and

    U μ , a ( x ) λ μ , a 1 2 p u μ , a x λ μ , a ,

    then U μ , a U in H 1 ( R 2 ) as a 0 + .

  3. v μ v in H 1 ( R 2 ) as μ 0 + , where v is a ground-state solution of Problem (1.2) for κ > κ 0 .

  4. w a , μ 0 in H 1 ( R 2 ) as a 0 + . Moreover, w a , μ w in H 1 ( R 2 ) as μ 0 + , where w is also a ground-state solution of Problem (1.2) for κ > κ 1 .

Remark 1.1

To consider the asymptotic behavior of solution in Theorem 1.3(ii), we are inspired by the results of [21, Section 4], where the key points are proving that λ μ , a 0 as a 0 + and the uniform boundedness of u μ , a . However, in our case, the nonlinearity is Moser-Trudinger critical growth at infinity and there is no corresponding limit equation at infinity. And thus, we cannot deduce the uniform boundedness of u μ , a as that in [21], where the nonlinearity is subcritical growth at infinity and there is the corresponding limit equation at infinity. We have to take a different way to attack it.

Remark 1.2

As a reference model, take

F ( t ) = κ t q e 3 π t 2 , t R , q > 4 ,

which satisfies ( f 5 ) ( f 8 ) . One can check that

f ( t ) t = κ q t q e 3 π t 2 + 6 π κ t q + 2 e 3 π t 2 θ κ t q e 3 π t 2 > 0 , t 0 , 4 < θ < q ,

and the function t K ( t ) t 4 K ( t ) t p is strictly increasing in ( 0 , ) , where

K ( t ) = f ( t ) t 2 F ( t ) = ( q 2 ) κ t q e 3 π t 2 + 6 π κ t q + 2 e 3 π t 2 .

2 Preliminaries

In what follows, we make use of the following notations.

  • H 1 ( R 2 ) stands for the usual Sobolev space endowed with the usual norm

    u 2 = R 2 ( u 2 + u 2 ) d x .

  • Denote by L p ( R 2 ) the usual Lebesgue space endowed with the norm

    u p p = R 2 u p d x , for all p [ 1 , + ) and u = ess sup x R 2 u ( x ) .

  • H r 1 ( R 2 ) = { u H 1 ( R 2 ) : u is radial } .

  • , denotes the action of dual.

  • C r , 0 ( R N ) denotes the space of continuous radial functions vanishing at .

  • C , C ε , C i , i N stand for positive constants that may depend on some parameters and whose precise value may change from line to line.

Now, to deal with the Moser-Trudinger critical nonlinearities, we recall some results about the well-known Moser-Trudinger inequality. Trudinger [35] proved that for any bounded open domain Ω R 2 , one has

sup u H 0 1 ( Ω ) , Ω u ( x ) 2 d x 1 Ω e α u 2 d x < + ,

for some exponent α > 0 . Subsequently, Moser [27] established a sharp form of aforementioned inequality. Then, Cao [8] proved the following Moser-Trudinger inequality in the whole space R 2 ,

(2.1) R 2 ( e α u 2 1 ) d x < + , for all u H 1 ( R 2 ) , α > 0 .

Moreover, if α < 4 π and u 2 M , there exists a constant C ( M , α ) > 0 , which depends only on M and α , such that

(2.2) sup u 2 1 R 2 ( e α u 2 1 ) d x C ( M , α ) .

For further results, we also refer to [9]. It follows from ( f 1 ) ( f 2 ) that for any ε > 0 , there exists positive constant C ε > 0 such that

F ( t ) ε t 4 + C ε t 4 ( e 4 π t 2 1 ) , for any t R .

Thus, by (2.1) and the Sobolev embedding, we have F ( u ) L 1 ( R 2 ) for all u H 1 ( R 2 ) . Therefore, the energy functional E μ : H 1 ( R 2 ) R is well defined and of C 1 -class by a standard argument. Set

(2.3) Λ ( a ) { u H 1 ( R 2 ) : P μ ( u ) = 0 and u S ( a ) } ,

where

P μ ( u ) = R 2 u 2 d x ( p 2 ) μ p R 2 u p d x R 2 f ( u ) u 2 F ( u ) d x .

Lemma 2.1

Let β > 0 and s > 1 . Then, for each α > s , there exists a positive constant C = C ( α ) such that for all t R ,

( e β t 2 1 ) s C ( e α β t 2 1 ) .

In particular, ( e β u 2 1 ) s belongs to L 1 ( R 2 ) for any u H 1 ( R 2 ) .

Proof

See the proof in [13, Lemma 2.2].□

For any u S ( a ) , we denote

u t ( x ) = t u ( t x ) , t > 0 ,

and

Ψ u ( t ) = E μ ( u t ) = t 2 2 R 2 u 2 d x t p 2 μ p R 2 u p d x t 2 R 2 F ( t u ) d x .

Then Ψ u ( t ) t = P μ ( u t ) by simple calculation.

Lemma 2.2

Let u S ( a ) be arbitrary but fixed, then we have

  1. u t 2 0 and E μ ( u t ) 0 , as t 0 ,

  2. u t 2 + and E μ ( u t ) , as t + .

Proof

By a straightforward calculation, it follows that

R 2 u t 2 d x = a 2 , R 2 u t s d x = t s 2 R 2 u ( x ) s d x , for all s 2 ,

and

R 2 u t 2 d x = t 2 R 2 u 2 d x .

For any fixed s > 2 , we have

(2.4) u t 2 0 and u t s 0 , as t 0 .

It follows from ( f 5 ) ( f 6 ) that for any ε > 0 , there exist C ε > 0 and s > 4 such that

(2.5) F ( t ) ε t 4 + C ε t s ( e 4 π t 2 1 ) , t R .

By (2.2) and (2.7),

(2.6) R 2 F ( u ) d x ε R 2 u 4 d x + C 1 R 2 u s ( e 4 π u 2 1 ) d x ε R 2 u 4 d x + C ε R 2 ( e 4 π u 2 1 ) 2 d x 1 2 R 2 u 2 s d x 1 2 ε u 4 4 + C u 2 s s R 2 ( e 12 π u 2 1 ) d x 1 2 .

Recall the famous Gagliardo-Nirenberg inequality [34, Lemma 2.4],

(2.7) u p p C ( N , p ) u 2 ( 1 r ) p u 2 r p , for any u H 1 ( R N ) , N 2 ,

where r = N ( 1 2 1 p ) . According to (2.4), it follows that

R 2 F ( u t ) d x 0 , as t 0 ,

and then

E μ ( u t ) 0 , as t 0 .

In order to show ( i i ) , note that as t + , u t 2 + and

E μ ( u t ) 1 2 u t 2 2 κ R 2 u t q d x = t 2 2 R 2 u 2 d x κ t q 2 R 2 u q d x ,

where we used the fact that q > 4 .□

3 Subcritical case: 2 < p < 4

In this section, we discuss the case 2 < p < 4 .

Lemma 3.1

For every u S ( a ) , the function Ψ u has exactly two critical points t u and t u + with 0 < t u < t u + . Moreover,

  1. t u is a local minimum point for Ψ u ( t ) = E μ ( u t ) , Ψ u ( u t u ) < 0 , and u t u V ( a ) ;

  2. t u + is a global maximum point for Ψ u , Ψ u ( t ) < 0 for all t > t u + and

    E μ ( u t u + ) inf u V ( c ) E μ ( u ) > 0 ,

where the sets V ( a ) and V ( a ) are given by

V ( a ) { u S ( a ) : u 2 < ρ } , V ( a ) { u S ( a ) : u 2 = ρ } ,

for a suitable constant ρ > 0 .

Proof

In view of the Gagliardo-Nirenberg inequality, one has

(3.1) u 2 s s C ( s ) u 2 s 1 u 2 , for all u H 1 ( R 2 ) , s [ 4 , + ) .

Let 0 < ρ 1 6 and μ ρ 4 p + ε for some ε > 0 . From (2.2), (2.6), and (3.1), one has

(3.2) E μ ( u ) 1 2 u 2 2 C ( p ) μ a 2 p u 2 p 2 ε C ( 4 ) a 2 u 2 2 C a u 2 s 1 1 4 ρ 2 C ( p ) a 2 μ p ρ p 2 a C ρ s 1 ρ 2 1 4 C 1 ρ ε C 2 ρ s 3 > 1 8 ρ 2 ,

for small enough ρ . Because Ψ u ( t ) 0 , u t 2 0 as t 0 and Ψ u ( t ) = E μ ( u t ) > 0 when u t V ( a ) = { v S ( a ) : v 2 2 = ρ 2 > 0 } . Necessarily, Ψ u has a first zero t u > 0 corresponding to a local minima. In particular, u t u V ( a ) and Ψ u ( t u ) < 0 . Now, from Ψ u ( t u ) < 0 , Ψ u ( t ) > 0 when u t V ( a ) and Ψ u ( t ) as t , Ψ u has a second zero t u + > t u corresponding to a local maxima of Ψ u with E μ ( u t u + ) inf u V ( a ) E μ ( u ) > 0 . To conclude the proofs of (i) and (ii), it just suffices to show that Ψ u has at most two zeros. However, this is equivalent to show that

θ ( t ) Ψ u ( t ) t = R 2 u 2 d x ( p 2 ) t p 4 μ p R 2 u p d x t 4 R 2 f ( t u ) t u 2 F ( t u ) d x

has at most two zeros. Note that

lim t 0 θ ( t ) , lim t + θ ( t ) ,

and there exists t * > 0 such that θ ( t * ) > 0 from (3.2). Since ( f 8 ) ,

θ ( t ) = t p 5 ( p 2 ) ( 4 p ) μ p R 2 u p d x t p R 2 K ( t u ) t u 4 K ( t u ) d x

has a unique zero point, which implies that θ ( t ) has indeed at most two zero points.□

Set μ 0 * = ρ 4 p + ε for some ε > 0 , where ρ is given in Lemma 3.1. As μ < μ 0 * , there exists a set V ( a ) S ( a ) having the property that

m μ ( a ) inf u V ( a ) E μ ( u ) < 0 < inf u V ( a ) E μ ( u ) .

It is well known, see, for example, [17, Lemma 2.7], that all critical points of E μ restricted to S ( a ) and thus any solution to problem ( P ) satisfies P μ ( u ) = 0 . Introducing the set

Λ ( a ) { u S ( a ) : P μ ( u ) = 0 } .

We shall show, see Lemma 3.1, that it admits the decomposition into the disjoint union Λ ( a ) = Λ ( a ) Λ + ( a ) , where

Λ ( a ) { u Λ ( a ) : E μ ( u ) < 0 } and Λ + ( a ) { u Λ ( a ) : E μ ( u ) > 0 } .

We say that u is a ground-state of problem ( P ) on S ( a ) if it is a solution to problem ( P ) having minimal energy among all the solutions which belongs to S ( a ) :

E μ S ( a ) ( u ) = 0 and E μ ( u ) = inf { E μ ( v ) : E μ S ( a ) ( v ) = 0 and v S ( a ) } .

We will show that

Proposition 3.1

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold. Then, E μ restricted to S ( a ) has a positive and radial ground-state for any μ < μ 0 * . This ground-state is a (local) minimizer of E μ in the set V ( a ) . In addition, any ground-state for E μ on S ( a ) is a local minimizer of E μ on V ( a ) .

Proof

From the definition of m μ ( a ) , there exists a minimizing sequence { u n } V ( a ) such that E μ ( u n ) m μ ( a ) as n . For any fixed n , denoting by v n the Schwarz rearrangement of u n . For more details, we refer readers to [6,26]. It follows from Lemma 3.1 and the property of v n that v n S ( a ) V ( a ) and { v n } is also the minimizing sequence. Note that, { v n } is bounded in H 1 ( R 2 ) . Indeed, there exists v V ( a ) such that as n , v n v in H 1 ( R 2 ) and v n v in L q ( R 2 ) , q ( 2 , + ) . By (2.2), we have

R 2 ( e 4 π v n 2 1 ) 2 d x C R 2 ( e 12 π v n 2 1 ) d x < + .

Note that

v n 2 2 ρ 2 < 1 6 ,

and v n converges almost everywhere to v in R 2 , we can see that e 4 π v n 2 ( x ) 1 converges almost everywhere to e 4 π v 2 ( x ) 1 in R 2 . This implies that

e 4 π v n 2 1 e 4 π v 2 1 , in L 2 ( R 2 ) ,

and thus,

R 2 v n s ( e 4 π v n 2 1 ) d x R 2 v s ( e 4 π v 2 1 ) d x ,

where we use the fact that v n v in L 2 s ( R 2 ) . By (2.5), the general Lebesgue control convergence theorem deduces that

(3.3) R 2 μ v n p p + F ( v n ) d x R 2 μ v p p + F ( v ) d x .

From the weak lower semicontinuity of the norm, we have

0 > m μ ( a ) liminf E μ ( v n ) E μ ( v ) ,

which implies that v 0 . Note that v 2 a . If v 2 = a , combining with E μ ( v ) m μ ( a ) , then, in view of the Lagrange multiplier theorem, there exists λ v R such that

E μ ( v ) + λ v v = 0 .

In fact,

0 > m μ ( a ) = E μ ( v ) 1 2 E μ ( v ) , v + λ v R 2 v 2 d x = 1 2 λ v R 2 v 2 d x + ( p 2 ) μ 2 p R 2 v p d x + R 2 1 2 f ( v ) v F ( v ) d x ,

we can deduce that λ v > 0 . Moreover, one can see that v is non-negative. The maximum principle [15] gives us that v > 0 on R N and this completes the proof.

If not, there is t = v 2 a < 1 such that

(3.4) R 2 v ( t x ) 2 d x = R 2 v 2 d x and R 2 u ( t x ) 2 d x = t 2 R 2 v 2 d x = a 2 .

Moreover,

m μ ( a ) E μ ( v ( t x ) ) = R 2 v 2 d x t 2 R 2 μ v p p + F ( v ) d x < R 2 v 2 d x R 2 μ v p p + F ( v ) d x m μ ( a ) .

This contradiction deduces that v 2 = a .

Set

{ u : E μ S ( a ) ( u ) = 0 and u S ( a ) } and c μ ( a ) = inf u E μ ( u ) ,

so that c μ ( a ) m μ ( a ) . For any w , consider

Ψ w ( t ) = E μ ( w t ) = t 2 2 R 2 w 2 d x μ t p 2 p R 2 w p d x t 2 R 2 F ( t w ) d x ,

and then, there exists 0 < t w < t w + such that m μ ( a ) Ψ w ( t w ) < 0 < Ψ w ( t w + ) and Ψ w ( t w ) = Ψ w ( t w + ) = 0 . Since w Λ ( a ) , one can see t w = 1 or t w + = 1 , which implies that

m μ ( a ) c μ ( a ) .

This deduces that m μ ( a ) = c μ ( a ) , and then, the ground-state is a (local) minimizer v of E μ in the set V ( a ) .

In addition, any ground-state z for E μ on S ( a ) . In fact, Λ ( a ) V ( a ) . If there exist u Λ ( a ) and u V ( a ) , from Lemma 3.1, we can find t u and t u + satisfying u t u Λ ( a ) and u t u + Λ + ( a ) . Since u V ( c ) , also from Lemma 3.1, one can see that t u < 1 < t u + , and then, Ψ u ( t ) has exactly three critical points t u , 1, and t u + , which contradicts Lemma 3.1. So z V ( a ) from z Λ ( a ) , and then, z is a local minimizer of E μ on V ( a ) . This completes the proof.□

The ground-state u a S ( a ) obtained in Proposition 3.1 lies on Λ ( a ) and can be characterized by

E μ ( u a ) = inf u Λ ( a ) E μ ( u ) = inf u V ( a ) E μ ( u ) = m μ ( a ) .

We denote by H r 1 ( R 2 ) the subspace of functions in H 1 ( R 2 ) , which are radially symmetric with respect to the origin and define S r ( a ) S ( a ) H r 1 ( R 2 ) . Accordingly, we also set Λ r ( a ) = Λ ( a ) H r 1 ( R 2 ) and Λ r + ( a ) = Λ + ( a ) H r 1 ( R 2 ) . In fact, similar to Proposition 3.1, Λ r ( a ) V ( a ) . Let

(3.5) M μ ( a ) inf h Γ 0 ( a ) max t [ 0 , 1 ] E μ ( h ( t ) ) ,

where

Γ 0 ( a ) { h C ( [ 0 , 1 ] , S r ( a ) ) : h ( 0 ) Λ r ( a ) , and E μ ( h ( 1 ) ) < 2 m μ ( a ) } .

In particular, if h Γ 0 ( a ) , then

h ( 0 ) 2 2 < ρ 2 < h ( 1 ) 2 2 ,

and by the mean value theorem, there exists t ¯ ( 0 , 1 ) such that h ( t ¯ ) 2 2 = ρ 2 . At the point τ ¯ ,

ρ 2 8 E μ ( h ( t ¯ ) ) sup τ [ 0 , 1 ] E μ ( h ( t ) ) .

Since h Γ 0 ( a ) is arbitrary, this implies that M μ ( a ) ρ 2 8 . We also note that the critical level satisfies M μ ( a ) < . We follow the strategy introduced in [17] and consider the functional E ˜ μ : R × H 1 ( R 2 ) R defined by

E ˜ μ ( t , u ) E μ ( u e t ) = Φ u ( t ) = e 2 t 2 R 2 u 2 d x μ e ( p 2 ) t p R 2 u p d x e 2 t R 2 F ( e t u ) d x .

Note that

t E ˜ μ ( t , u ) = Φ u ( t ) = 1 e t P μ ( u e t ) ,

and, for any v H 1 ( R 2 ) ,

u E ˜ μ ( t , u ) ( v ) = e 2 t R 2 u v d x μ e ( p 2 ) t R 2 u p 2 u v d x e 2 t R 2 f ( e t u ) e t v d x = E μ ( u e t ) ( v e t ) .

For this proof, we refer the reader to see [18, Lemma 3.1]. Given a > 0 , we say that

M ˜ μ ( a ) inf h ˜ Γ ˜ ( a ) max t [ 0 , 1 ] E ˜ μ ( h ˜ ( t ) ) > max { E ˜ μ ( h ˜ ( 0 ) ) , E ˜ μ ( h ˜ ( 1 ) ) } ,

where

Γ ˜ ( a ) { h ˜ C ( [ 0 , 1 ] , R × S r ( a ) ) : h ˜ ( 0 ) ( 0 , Λ r ( a ) ) , and E ˜ μ ( h ˜ ( 1 ) ) < 2 m μ ( a ) } .

Let h Γ 0 ( a ) , since h ˜ ( t ) = ( 0 , h ( t ) ) Γ ˜ ( a ) , and E ˜ μ ( h ˜ ( t ) ) = E μ ( h ( t ) ) for all t R , we have that M μ ( a ) M ˜ μ ( a ) . Next, we shall prove that M ˜ μ ( a ) M μ ( a ) . For all h ˜ ( t ) = ( s ( t ) , v ( t ) ) Γ ˜ ( a ) , setting h ( t ) = ( v t ) e s ( t ) , and then, we have that h : [ 0 , 1 ] S r ( a ) is continuous and

h ( 0 ) Λ r ( a ) and E μ ( h ( 1 ) ) < 2 m μ ( a ) .

Hence, h Γ 0 ( a ) and E ˜ μ ( h ˜ ( t ) ) = E μ ( ( v t ) e s ( t ) ) = E μ ( h ( t ) ) . Thus, M ˜ μ ( a ) M μ ( a ) , and finally,

M μ ( a ) = M ˜ μ ( a ) .

Proposition 3.2

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold. Then, there exists a Palais-Smale sequence { u n } S r ( a ) for E μ restricted to S r ( a ) at level M μ ( a ) with P μ ( u n ) 0 as n .

Proof

Following [14, Sect. 5], we set

  1. = { h ˜ ( [ 0 , 1 ] ) : h ˜ Γ ˜ ( a ) } ,

  2. B = ( 0 , Λ r ( a ) ) ( 0 , a ) , with a { u S r ( a ) : E μ ( u ) < 2 m μ ( a ) } ,

  3. D = { ( s , u ) R × S r ( a ) : E ˜ μ ( s , u ) M ˜ μ ( a ) } .

Since E ˜ μ has a mountain pass geometry at level M ˜ μ ( a ) (see Lemma 3.1) and by the definition of the superlevel set D , we obtain D \ B = D and

sup ( s , u ) B E ˜ μ ( s , u ) M ˜ μ ( a ) inf ( s , u ) D E ˜ μ ( s , u ) .

For any A , there exists a h 0 Γ ˜ ( a ) such that A = h 0 ( [ 0 , 1 ] ) and

M ˜ μ ( a ) = inf h ˜ Γ ˜ ( a ) max t [ 0 , 1 ] E ˜ μ ( h ˜ ( t ) ) max t [ 0 , 1 ] E ˜ μ ( h 0 ( t ) ) .

Hence, there exists a t 0 [ 0 , 1 ] such that M ˜ μ ( a ) E ˜ μ ( h 0 ( t 0 ) ) . This means that h 0 ( t 0 ) D , and consequently,

A D \ B , for all A .

Now, for all ( s , u ) R × S r ( a ) , we have

E ˜ μ ( s , u ) = E μ ( u e s ) = E μ ( u e s ) = E ˜ μ ( 0 , u e s ) .

Hence, for any minimizing sequence { z n = ( α n , β n ) } Γ ˜ ( a ) for M ˜ μ ( a ) , the sequence

{ y n = ( 0 , β n e α n ) }

is also a minimizing sequence for M ˜ μ ( a ) .

Using the terminology in [14, Sect. 5], it means that is a homotopy stable family of compact subset of R × S r ( a ) with extended closed boundary B and the superlevel set D is a dual set for . By [14, Theorem 5.2] with the minimizing sequence { y n } , there exists a Palais-Smale sequence { ( s n , w n ) } R × S r ( a ) for E ˜ μ restricted to R × S r ( a ) at level M ˜ μ ( a ) , i.e., as n ,

(3.6) s E ˜ μ ( s n , w n ) 0

and

(3.7) u E ˜ μ ( s n , w n ) ( T w n S r ( a ) ) * 0 ,

where T w n S r ( a ) v S r ( a ) : R 2 w n v d x = 0 , so that

(3.8) s n 0 + w n β n e α n 0 ,

which deduces that { s n } is bounded. Then, by (3.6), we obtain 1 e s n P μ ( ( w n ) e s n ) 0 as n . Also, (3.7) implies that

E ˜ μ ( ( w n ) e s n ) ( ϕ e s n ) 0 ,

as n , for every ϕ T w n S r ( a ) . Let u n ( w n ) e s n , then we obtain that { u n } S r ( a ) is a Palais-Smale sequence for E ˜ μ restricted to S r ( a ) at level M μ ( a ) , with P μ ( u n ) 0 . Since the problem is invariant under rotations, { u n } S r ( a ) is also the Palais-Smale sequence for E μ restricted to S ( a ) at level M μ ( a ) , with P μ ( u n ) 0 .□

Proof of Theorem 1.1

Thanks to Proposition (3.1), it suffices to find the second solution. From Proposition (3.1), there exists a non-negative sequence { u n } H r 1 ( R 2 ) such that

E μ ( u n ) M μ ( a ) , E μ S ( a ) ( u n ) 0 , and P μ ( u n ) 0 .

We claim that there are two positive constants μ 0 and κ 0 such that

u n 2 2 1 4 ,

for any μ < μ 0 and κ > κ 0 , which implies that { u n } is bounded, and then, there exists u H r 1 ( R 2 ) such that as n , u n u in H 1 ( R 2 ) and u n u in L s ( R 2 ) , s ( 2 , + ) .

Also by (2.2) and Lemma 2.1, we have

R 2 ( e 4 π u n 2 1 ) 2 d x C R 2 ( e 12 π u n 2 1 ) d x < + .

Since u n converges almost everywhere to u in R 2 , e 4 π u n 2 ( x ) 1 converges almost everywhere to e 4 π u 2 ( x ) 1 in R 2 . This implies that e 4 π u n 2 ( x ) 1 e 4 π u 2 ( x ) 1 in L 2 ( R 2 ) . Then,

R 2 u n s ( e 4 π u n 2 1 ) d x R 2 u s ( e 4 π u 2 1 ) d x ,

where we use the fact that u n u in L 2 s ( R 2 ) . By (2.5), the general Lebesgue-dominated convergence theorem implies that

(3.9) R 2 μ ( p 2 ) p u n p + f ( u n ) u n 2 F ( u n ) d x R 2 μ ( p 2 ) p u p + f ( u ) u 2 F ( u ) d x .

Since P μ ( u n ) 0 , we have

R 2 u 2 d x liminf n R 2 u n 2 d x = liminf n ( p 2 ) μ p R 2 u n p d x R 2 f ( u n ) u n 2 F ( u n ) d x = ( p 2 ) μ p R 2 u p d x R 2 f ( u ) u 2 F ( u ) d x .

If u = 0 , combining with (3.9), we see that

(3.10) R 2 u n 2 d x = ( p 2 ) μ p R 2 u n p d x + R 2 f ( u n ) u n 2 F ( u n ) d x 0 ,

which implies that E μ ( u n ) 0 . It is impossible since M μ ( a ) > 0 . Thus, u 0 . From [7, Lemma 3], one can see that

(3.11) E μ ( u n ) + λ n u n 0 ,

where

λ n = 1 a 2 E μ ( u n ) , u n = 1 a 2 R 2 u n 2 d x μ R 2 u n p d x R 2 f ( u n ) u n d x .

Combining with (3.13), we have

(3.12) λ n = 1 a 2 R 2 u n 2 d x μ R 2 u n p d x R 2 f ( u n ) u n d x = 1 a 2 μ ( p 2 ) p R 2 u n p d x + R 2 f ( u n ) u n 2 F ( u n ) d x μ R 2 u n p d x R 2 f ( u n ) u n d x = 1 a 2 2 μ p R 2 u n p d x 2 R 2 F ( u n ) d x 1 a 2 2 μ p R 2 u p d x 2 R 2 F ( u ) d x .

From this, up to subsequence, still denoted by { λ n } , we can assume that

λ n λ > 0 , as n + .

Now, (3.11) implies that

E μ ( u ) + λ u = 0 , in R 2 .

Thus,

u 2 2 + λ u 2 2 = μ u p p + R 2 f ( u ) u d x .

On the other hand,

u n 2 2 + λ n u n 2 2 = μ u n p p + R 2 f ( u n ) u n d x + o n ( 1 ) .

Recalling that

μ R 2 u n p d x + R 2 f ( u n ) u n d x μ R 2 u p d x + R 2 f ( u ) u d x ,

we derive that

u n 2 2 + λ n u n 2 2 u 2 2 + λ u 2 2 .

Since λ > 0 , the last limit implies that

u n u , in H 1 ( R 2 )

deducing that u 2 2 = a 2 . This establishes the desired result.

Next, we prove that there exist μ 0 and κ 0 such that

u n 2 2 1 2 ,

for any μ < μ 0 and κ > κ 0 . Taking a fixed positive function w H 1 ( R 2 ) with w 2 2 = a 2 , and then for any t > 0 ,

max t > 0 E μ ( w t ) max t > 0 t 2 2 R 2 w 2 d x κ t q 2 R 2 w q d x C κ 2 4 q .

So that

C κ 2 4 q M μ ( a ) .

Using the fact that E μ ( u n ) = M μ ( a ) + o n ( 1 ) and P μ ( u n ) = o n ( 1 ) , it follows that

(3.13) M μ ( a ) + o ( 1 ) = ( θ 2 ) E μ ( u n ) P μ ( u n ) = θ 2 2 R 2 u n 2 d x ( θ 2 ) μ p R 2 u n p d x ( θ 2 ) R 2 F ( u n ) d x R 2 u n 2 d x + ( p 2 ) p μ α R 2 u p d x + R 2 f ( u n ) u n 2 F ( u n ) d x = θ 4 2 R 2 u n 2 d x + ( p θ ) μ p R 2 u n p d x + R 2 f ( u n ) u n θ F ( u n ) d x θ 4 2 u n 2 2 C μ ( θ p ) a 2 p u n 2 p 2 ,

which implies that there exist μ 0 * > μ 0 > 0 and κ 0 > 0 such that

u n 2 2 1 2 ,

for any μ < μ 0 and κ > κ 0 . This completes the proof.□

4 Critical case: p = 4

In this section, we discuss the case p = 4 .

Lemma 4.1

Assume that ( f 5 ) ( f 8 ) hold. Then, there exist a 1 > 0 or μ 1 > 0 such that if a a 1 or μ μ 1 , for any u S ( a ) , there exists a unique t u > 0 such that u t u Λ ( a ) .

Proof

Similar to Lemma 3.1, for any u S ( a ) , we define for t > 0 ,

Ψ ( t ) = E ( u t ) = t 2 2 R 2 u 2 d x μ t 2 4 R 2 u 4 d x t 2 R 2 F ( t u ) d x .

One can easily see that

P μ ( u t ) = Ψ ( t ) t = t 2 R 2 u 2 d x μ t 2 2 R 2 u 4 d x t 2 R 2 f ( t u ) t u 2 F ( t u ) d x .

There exists a 1 > 0 or μ 1 > 0 such that if a a 1 or μ μ 1 ,

1 2 u 2 2 μ 4 u 4 4 1 2 μ C a 2 u 2 2 > 0 ,

by the Gagliardo-Nirenberg inequality. Therefore, similar to Lemma 3.1, there exists t u > 0 such that Ψ ( t u ) = max t > 0 Ψ ( t ) and Ψ ( t u ) = 0 , i.e., P μ ( u t u ) = 0 and u t u Λ ( a ) .

Suppose that there exists t 1 > t 2 > 0 such that u t 1 Λ ( a ) and u t 2 Λ ( a ) . It follows from ( f 5 ) and ( f 8 ) that K ( t ) t > 4 K ( t ) > 0 , which implies that the function t K ( t ) t 4 is strictly increasing in ( 0 , ) . Then, one has

t 1 4 R 2 f ( t 1 u ) t 1 u 2 F ( t 1 u ) d x = 1 2 u 2 2 μ 4 u 4 4 = t 2 4 R 2 f ( t 2 u ) t u 2 F ( t 2 u ) d x ,

which is a contradiction. Hence, t u is unique.□

It follows from a standard argument (see [39]) that

M μ ( a ) inf u Λ ( a ) E μ ( u ) = inf u S ( a ) max t > 0 E μ ( u t ) ,

where Λ ( a ) is given in (2.3).

Lemma 4.2

Assume that ( f 5 ) ( f 8 ) hold, then

0 < M μ ( a ) C κ 2 4 q .

Proof

If u 2 2 1 4 , then by (2.6) and (3.1), P μ ( u ) = 0 means that

(4.1) u 2 2 = μ 2 u 4 4 + R 2 f ( u ) u 2 F ( u ) d x C ( 4 ) a 2 μ 2 u 2 2 + ε C ( 4 ) a 2 u 2 2 + C ( s ) a u 2 s 1 .

This shows that there exists 0 < ρ 1 4 such that u 2 2 ρ for any u Λ ( a ) . We observe that

(4.2) ( θ 2 ) E μ ( u ) = ( θ 2 ) E μ ( u ) P μ ( u ) = θ 4 2 u 2 2 + ( 4 θ ) μ 4 u 4 4 + R 2 f ( u ) u θ F ( u ) d x θ 4 2 u 2 2 ( 4 θ ) C μ a 2 4 u 2 2 .

Therefore, E μ ( u ) C ρ for any u Λ ( a ) if μ , small enough. This follows that M μ ( a ) > 0 .

On the other hand, it shows in [23] that there is a positive function w , which is the ground-state solution of the following problem:

(4.3) Δ w + w = w q 2 w , in R 2 , lim x w ( x ) = 0 .

Let v a w w 2 , then v t S a for any t > 0 and

max t > 0 E μ ( v t ) max t > 0 t 2 a 2 R 2 v 2 d x κ t q 2 a p 2 q R 2 v q d x C κ 2 4 q .

This completes the proof.□

Proof of Theorem 1.2

From the definition of M μ ( a ) , there exists a minimizing sequence { u n } Λ ( a ) such that E μ ( u n ) M μ ( a ) as n . For any fixed n , denoting by u n * the Schwarz rearrangement of u n , it follows from Lemma 4.1 and the property of u n * that u n * S ( a ) and there exists 0 < t n < 1 such that ( u n * ) t n Λ ( a ) . So E μ ( ( u n * ) t n ) E μ ( u n ) and v n ( u n * ) t n is also a minimizing sequence. Note that, { v n } is bounded in H 1 ( R 2 ) . Then, there exists v H 1 ( R 2 ) such that as n , v n v in H 1 ( R 2 ) , and v n v in L q ( R 2 ) , q ( 2 , + ) .

From (4.2), we can find

θ 4 2 v n 2 2 ( 4 θ ) C μ a 2 p v n 2 2 ( θ 4 ) M μ ( a ) + o ( 1 ) C κ 2 4 q ,

which deduces that there exists a 1 > 0 , μ 1 > 0 , and κ 1 > 0 such that 4 v n 2 2 < 1 if 0 < μ < μ 1 and κ > κ 1 , or 0 < a < a 1 and κ > κ 1 . Similarly, in the proof of Theorem 1.1, we have

(4.4) R 2 μ 2 v n 4 + f ( v n ) v n 2 F ( v n ) d x R 2 μ 2 v 4 + f ( v ) v 2 F ( v ) d x .

If v = 0 , combining with (4.4), we see that

(4.5) R 2 v n 2 d x = μ R 2 v n p d x + R 2 f ( v n ) v n 2 F ( v n ) d x 0 ,

which implies that E μ ( v n ) 0 . It is impossible since M μ ( a ) > 0 . Thus, v 0 . If

R 2 v 2 d x < R 2 v n 2 d x = a ,

then there is s > 1 such that

R 2 v ( x s ) 2 d x = s 2 R 2 v 2 d x = a and R 2 v ( x s ) 2 d x = R 2 v 2 d x .

Combining with (4.4), we have

R 2 v 2 d x μ s 2 R 2 v 2 d x + s 2 R 2 f ( v ) v 2 F ( v ) d x .

It follows from Lemma 3.1 that there exists 0 < t s < 1 such that ( v ( s ) ) t s Λ ( a ) . Then, we have

M μ ( a ) E μ ( ( v ( s ) ) t s ) = E μ ( v t s ) + μ t s 2 4 R 2 v 4 s 2 v 4 d x + t s 2 R 2 [ F ( t s v ) s 2 F ( t s v ) ] d x < E μ ( v t s ) liminf E μ ( ( u n ) t s ) liminf E μ ( ( u n ) ) M μ ( a ) ,

which is a contradiction. Thus, we obtain that v 2 2 = a .

In fact, v n v in H 1 ( R 2 ) . If not, by (4.4), we have

(4.6) v 2 2 < liminf n v n 2 2 = μ R 2 v p d x + R 2 f ( v ) v 2 F ( v ) d x .

Also, it follows from Lemma 3.1 that there exists 0 < t < 1 such that v t Λ ( a ) . Then,

M μ ( a ) E μ ( v t ) < liminf E μ ( ( u n ) t ) liminf E μ ( ( u n ) ) M μ ( a ) ,

which is a contradiction. Hence, v Λ ( a ) and E μ ( v ) = M μ ( a ) .

Assume that E μ S ( a ) ( v ) 0 , then there exist δ > 0 and ϱ > 0 such that

u S ( a ) , u v 3 δ E μ S ( a ) ( u ) ϱ ,

and

lim t 1 v t v = 0 .

Thus, there exists δ 1 ( 0 , 1 4 ) such that

t 1 < δ 1 v t v < δ .

Let ε min M μ ( a ) 4 , ϱ δ 8 and S v ( a ) B ( v , δ ) S ( a ) . Then, [39, Lemma 5.15] yields a deformation η C ( [ 0 , 1 ] × S ( a ) , S ( a ) ) such that

  1. η ( 1 , u ) = u if u E μ 1 [ M μ ( a ) 2 ε , M μ ( a ) + 2 ε ] S v ( a ) ,

  2. η ( 1 , E μ M μ ( a ) + ε S v ( a ) ) E μ M μ ( a ) ε ,

  3. E μ ( η ( , u ) ) is nonincreasing for every u S ( a ) . In particular, E μ ( η ( 1 , u ) ) E μ ( u ) .

Also from Lemma 4.1, we have

E μ ( v t ) E μ ( v ) = M μ ( a ) , for all t > 0 .

As t 1 < δ 1 , we know v t E μ M μ ( a ) + ε S v ( a ) . The second property of the mapping η means that

(4.7) E μ ( η ( 1 , v t ) ) M μ ( a ) ε , for all t 1 < δ 1 .

On the other hand, as in Lemma 4.1, we can see that

E μ ( v t ) max { E μ ( v 1 δ ) , E μ ( v 1 + δ ) } < E μ ( v ) , for all t 1 δ 1 .

Therefore one has

(4.8) E μ ( η ( 1 , v t ) ) E μ ( v t ) M μ ( a ) δ 2 ,

where δ 2 = E μ ( v ) max { E μ ( v 1 δ ) , E μ ( v 1 + δ ) } . Combining (4.7) with (4.8), we have

max t > 0 E μ ( η ( 1 , v t ) ) < M μ ( a ) .

From Lemma 2.2, there exist 0 < T 1 < T 2 such that

P μ ( v T 1 ) > 0 , P μ ( v T 2 ) < 0 , and max { E μ ( v T 1 ) , E μ ( v T 2 ) } < M μ ( a ) 2 ε .

So one can obtain that

P μ ( η ( 1 , v T 1 ) ) = P μ ( v T 1 ) > 0 and P μ ( η ( 1 , v T 2 ) ) = P μ ( v T 2 ) < 0 .

Since t P μ ( η ( 1 , v t ) ) is continuous in ( 0 , ) , we have that P μ ( η ( 1 , v t 0 ) ) = 0 for some t 0 > 0 , namely, η ( 1 , v t ) Λ ( a ) . So that

M μ ( a ) E μ ( η ( 1 , v t 0 ) ) max t > 0 E μ ( η ( 1 , v t ) ) < M μ ( a ) ,

which is a contradiction. Therefore, we can conclude that E μ S ( a ) ( v ) = 0 and there exists a Lagrange multiplier λ v > 0 such that ( v , λ v ) is a solution of problem ( P ).□

5 Asymptotic behavior of solution

Let u μ n , a k be the ground-state solution in Theorem 1.1 and E μ ( u μ n , a k ) = m μ n ( a k ) , where μ n 0 as n and a k 0 as k , respectively.

Lemma 5.1

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold, then m μ ( a ) 0 as μ 0 or a 0 .

Proof

In fact, for any u V ( a ) , one can see that u 2 < ρ . Similar to (3.2), one has

E μ ( u ) 1 2 u 2 2 C ( p ) μ a 2 p u 2 p 2 ε C ( 4 ) a 2 u 2 2 C a u 2 s 1 1 2 ε C ( 4 ) a 2 C ρ s 3 u 2 2 C ( p ) μ a 2 p u 2 p 2 C ( p ) μ a 2 p ρ p 2 .

So that 0 m μ ( a ) C ( p ) μ a 2 p ρ p 2 0 , as μ 0 or a 0 .□

Proposition 5.1

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold. For a fixed a k , then u μ n , a k 2 0 as n and the corresponding Lagrange multiplier λ μ n , a k 0 as n .

Proof

For a fixed a k , we donate u μ n , a k by u μ n for convenience. Using the fact that u μ n 2 ρ and

(5.1) ( θ 2 ) m μ n ( a ) = ( θ 2 ) E μ n ( u μ n ) P μ n ( u μ n ) θ 4 2 u μ n 2 2 C μ n ( θ p ) a 2 p u μ n 2 p 2 ,

which implies that u μ n 2 0 as n since Lemma (5.1). In fact, { u μ n } is bounded in H r 1 ( R 2 ) from (5.1), and then there exists u H r 1 ( R 2 ) such that as n , u μ n u in H 1 ( R 2 ) . If u 0 , as in the proof of Theorem 1.1, we have E 0 ( u ) + λ u u = 0 in R 2 for some λ u > 0 . Thus,

λ u R 2 u φ d x = R 2 f ( u ) φ d x , for any φ C 0 ( R 2 ) ,

contradicting with ( f 7 ) and then u = 0 . Furthermore, one can see λ μ n 0 from the definition of λ μ n .□

Lemma 5.2

Assume that 2 < p < 4 and ( f 5 ) ( f 8 ) hold. Let ( u , λ ) be the solution of problem ( P ) with λ > 0 and u 2 1 2 , then u L ( R 2 ) .

Proof

We shall use the Brézis-Kato estimate and Moser iteration technique to show it. Let ( u , λ ) H 1 ( R 2 ) × R + be a solution of problem ( P ) and M > 0 , where u 2 1 2 . Define

(5.2) u M ( x ) u ( x ) , if u ( x ) M , M , if u ( x ) > M , M , if u ( x ) < M .

Let v u M 2 α u H 1 ( R 2 ) and α > 0 , multiplying both sides of Problem (1.1) with v and integrating over R 2 , we have

R 2 u ( u M 2 α u ) d x + λ R 2 u M 2 α u 2 d x = R 2 μ u p u M 2 α + f ( u ) u M 2 α u d x .

It follows from ( f 5 ) ( f 6 ) that there exist C λ > 0 and s > 4 such that

(5.3) R 2 μ u p u M 2 α + f ( u ) u M 2 α u d x λ 2 R 2 u 2 u M 2 α d x + C λ u s u M 2 α 2 R 2 ( e 12 π u 2 1 ) d x 1 2 λ 2 R 2 u 2 u M 2 α d x + C R 2 ( u s u M 2 α ) 2 d x 1 2 ,

where we also use (2.7), which together with the Sobolev inequality yields

1 ( α + 1 ) 2 u M α + 1 4 s 2 C R 2 u s u M 2 α 2 d x 1 2 C R 2 u 2 s d x 2 s 4 4 s R 2 u M 2 s α u 2 s d x 1 s ,

where r = 1 1 2 s . Thus,

u 4 s ( α + 1 ) 2 ( α + 1 ) [ C ( α + 1 ) 2 ] u 2 s 2 2 s u 2 ( s 2 ) ( 1 1 2 s ) u 2 s ( α + 1 ) 2 ( α + 1 ) ,

and then,

u 4 s ( α + 1 ) [ C ( α + 1 ) ] 1 α + 1 u 2 s 2 4 s ( α + 1 ) u 2 ( s 2 ) ( 1 1 2 s ) 2 ( α + 1 ) u 2 s ( α + 1 ) .

Next, we will use the Moser iteration. For all n N , set

(5.4) b n 1 = 2 b n , n > 0 , b n = α n + 1 , 1 ( α 1 + 1 ) 2 λ 2 ,

i.e.,

b n = 2 n 1 ( a 1 + 1 ) , for all n = 1 , 2 , .

Combining with (5.4), we have

(5.5) u 4 s b n [ C b n ] 1 b n u 2 ( s 2 ) 4 s b n u 2 ( s 2 ) ( 1 1 2 s ) 2 b n u 2 s b n C 1 n 1 b i i = 1 n b i 1 b i u 2 i = 1 n s 2 4 s b i u 2 i = 1 n ( s 2 ) ( 1 1 2 s ) 2 b i u 2 s b 1 .

Let δ i = [ C b n ] 1 b n , one can obtain that

θ n ln i = 1 n δ i = i = 1 n ln [ C ( a 1 + 1 ) 2 n 1 ] 2 n 1 ( a 1 + 1 ) θ , as n ,

and ρ n = i = 1 n 1 b i . Clearly, lim n ρ n = ρ < . Then, let n in (5.5), one can earn

(5.6) u e θ u 2 s 2 4 s ρ u 2 ( s 2 ) ( 1 1 2 s ) 2 ρ u 2 s b 1 < + .

Therefore, from (5.6), we obtain that u L ( R 2 ) . This completes the proof.□

Proof of Theorem 1.3

Let u μ n , a k be the ground-state solution in Theorem 1.1, where μ n 0 as n and a k 0 as k , respectively. From Proposition 5.1, we can obtain the asymptotic behavior of u μ n , a k in Theorem 1.3(i)

For convenience, we denote u μ n , a k by u k for a fixed μ n . Similarly, the corresponding Lagrange multiplier λ μ n , a k is denoted by λ k . In fact, (5.1) and Lemma (5.1) read that u k 2 0 as k . Combining with the definition of λ k , one can see λ k 0 + . Since u k H r 1 ( R 2 ) , from [28,33], one can see that

u k ( x ) 0 , as x , uniformly in k N .

Similar to the proof of [22, Theorem 12.2.2], it shows that u k W loc 2 , 2 ( R 2 ) according to Lemma 5.2. After passing to a subsequence of { ( u k , λ k ) } , the Sobolev embedding theorem implies that there exists M > 0 such that

u k M , uniformly in k N .

So { ( u k , λ k ) } also solve the following Schrödinger equation:

(5.7) Δ u + λ u = μ u p 2 u + χ ( u ) f ( u ) , in R 2 , u ( x ) 0 , u H 1 ( R 2 ) ,

having prescribed mass

R 2 u 2 d x = a 2 > 0 ,

where χ C 0 ( [ 0 , + ) ) satisfies

(5.8) χ ( t ) = 1 , 0 t M , 0 , t 2 M .

Set g ( s ) = μ s p 2 s + χ ( s ) f ( s ) , so that g C 1 ( [ 0 , + ) ) , g ( s ) > 0 for s > 0 and

lim s 0 + g ( s ) s p 2 = μ ( p 1 ) > 0 and lim s + g ( s ) s p 2 = μ ( p 1 ) > 0 .

Therefore, g satisfies the nonlinear conditions ( G 1 ) and ( G 2 ) assumed in [21]. Moreover, [21, Remark 2.6] gives us that, based on ( G 1 ) and ( G 2 ) , the condition ( G 3 ) will hold automatically,

  1. Δ u = g ( u ) has no positive radial decreasing classical solution in R 2 .

Hence, similarly by [21, Theorem 4.6], we directly deduce Theorem 1.3-(ii).

Let v μ n and w a m , μ n be the mountain path-type solution in Theorems 1.1 and 1.2 such that E μ ( v μ n ) = M μ n ( a ) and E μ ( w a m , μ n ) = M a m , μ n ( a m ) , respectively. Here, μ n 0 as n and a m 0 as m .

Since E μ ( u ) E 0 ( u ) for any u H 1 ( R 2 ) , we obtain that

limsup n 0 M μ n ( a ) M 0 ( a ) .

Indeed, { v μ n } is bounded from (3.13). From Lemma 3.1, we have

liminf n 0 M μ n ( a ) = liminf n 0 max t > 0 E μ ( ( v μ n ) t ) = max t > 0 E 0 ( ( v μ n ) t ) + o ( 1 ) M 0 ( a ) + o ( 1 ) .

Then, lim n 0 M μ n ( a ) = M 0 ( a ) . Note that v μ n 2 2 1 4 , as in the proof of Theorem 1.1, v μ n v in H 1 ( R 2 ) , the corresponding Lagrange multiplier λ n v μ n λ v < 0 and E 0 ( v ) = M 0 ( a ) . It follows from [2] that v is the ground-state solution of Problem (1.2) for κ > κ 0 .

Similarly, we obtain that w a m , μ n w in H 1 ( R 2 ) and λ n w a m , μ n λ w < 0 as n and E 0 ( w ) = M 0 ( a m ) , where lim n 0 M μ n ( a m ) = M 0 ( a m ) . Also from [2], one can see that w is the ground-state solution of Problem (1.2) for κ > κ 1 .

In fact, w a m , μ n 2 2 1 4 . According to (3.1), as m , we have

w a m , μ n s s C ( s ) w a m , μ n 2 s 2 w a m , μ n 2 2 0 , s [ 2 , + ) .

Moreover, as in the proof of Theorem 1.1, P μ ( w a m , μ n ) = 0 implies that

R 2 w a m , μ n 2 d x = ( p 2 ) μ p R 2 w a m , μ n p d x + R 2 f ( w a m , μ n ) w a m , μ n 2 F ( w a m , μ n ) d x 0 ,

which deduces that w a m , μ n 0 in H 1 ( R 2 ) as m 0 . This completes the proof.□

Acknowledgement

The authors thank the referees for their valuable suggestions and comments on the manuscript.

  1. Funding information: Gui-Dong Li was supported by the special (special post) scientific research fund of Natural Science of Guizhou University (No. (2021)43), Guizhou Provincial Education Department Project (No. (2022)097), Guizhou Provincial Science and Technology Projects (No. [2023]YB033, [2023]YB036), and National Natural Science Foundation of China (No. 12201147). Jianjun Zhang was supported by National Natural Science Foundation of China (No. 12371109, 11871123).

  2. Author contributions: Zhang proposed the idea for the study and led the implementation review and revision of the manuscript. Li proposed research ideas and writing – original draft preparation. All authors have read and agreed to the published version of the manuscript.

  3. Conflict of interest: The authors state no conflict of interest.

  4. Data availability statement: Data sharing is not applicable to this article as no datasets were generated or analyzed during the current study.

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Received: 2023-10-07
Revised: 2024-04-28
Accepted: 2024-05-27
Published Online: 2024-07-02

© 2024 the author(s), published by De Gruyter

This work is licensed under the Creative Commons Attribution 4.0 International License.

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